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Removal of the lower bungee cable as indicated in the attached sketch.
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Lengthening of the seat guide in order to effect a more positive engagement of the seat at the front attaching point.
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There is now available a kit number 752-186 to install the auxiliary fuel line in the Piper Pacer "115", "125" and "135".
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Recommendation that two hinge plates, Part Number 11876-00, be installed on the fuselage door hinge as an added safety feature to prevent the rivets from working loose.
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Changing the stabilizer adjustment cable fiber rub block to a pulley arrangement to prevent cable slippage and possible cable fraying.
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Instructions to eliminate slackness in both the right and left rudder cables.
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It is recommended that a #6 x 3/8" Parker Screw be installed in the rudder pedal tube clamp of the right hand rudder pedals to eliminate the possible rotation of the rudder pedal cross tube on the torque tube arm.
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Inspection of the aluminum fuel lines forward of the fuel valve.
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Inspecting the entire muffler assembly and tailpipe for cracks in PA-11 aircraft.
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Inspection of upper and lower shock strut end fitting attachment bolts for excessive tightness.